A boundary integral formulation for predicting acoustic waves generated by large deformations of bodies

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Massimo Gennaretti, Beatrice De Rubeis
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引用次数: 0

Abstract

This paper presents the application and assessment of a recently introduced boundary integral formulation for solving wave equations in domains bounded by porous or solid surfaces undergoing large deformations. Specifically, it is applied to predict acoustic waves generated by large-amplitude pulsations of a sphere immersed in an unbounded, quiescent, inviscid perfect gas. Fluid perturbations are expressed in terms of the velocity potential. The focus is on the assessment of the capability of the integral formulation to capture the effects induced by significant boundary deformations. To isolate these effects, fluid nonlinearities are neglected, as their contributions are given by field volume terms and fall outside the scope of this study. The numerical application of the boundary integral formulation is accomplished by a zero-th order boundary element method, complemented by a novel harmonic-balance approach for time integration. This innovative approach provides an efficient and robust solution method for handling periodic perturbation propagation phenomena. For a wide range of amplitudes and frequencies of sphere oscillation, the deformable-boundary integral formulation solving the linear wave equation for the velocity potential is validated against analytical linear solutions. In the case of large-amplitude, high-frequency pulsations the analytical solution, not available in the literature, is derived in this work under subsonic surface speed conditions. Numerical results highlight the multi-harmonic nature of the radiated acoustic field and provide an analysis of the boundary contributions associated with surface dynamic deformation. Successful applications to porous deforming spherical and wing-like shaped boundaries are also presented for the sake of completeness.
预测物体大变形所产生的声波的边界积分公式
本文介绍了最近引入的一种边界积分公式的应用和评价,用于求解大变形的多孔或固体表面边界域中的波动方程。具体地说,它被用于预测浸入无界的、静止的、无粘性的完美气体中的球体的大振幅脉动所产生的声波。流体扰动用速度势表示。重点是评估积分公式的能力,以捕捉由显著的边界变形引起的影响。为了分离这些影响,流体非线性被忽略,因为它们的贡献是由场体积项给出的,不属于本研究的范围。边界积分公式的数值应用是通过零阶边界元法完成的,并辅以一种新的时间积分的谐波平衡方法。该方法为处理周期性扰动传播现象提供了一种高效、鲁棒的求解方法。对于较大范围的球振动振幅和频率,用解析线性解验证了求解速度势线性波动方程的变形边界积分公式。在大振幅、高频脉动的情况下,本文在亚音速表面速度条件下推导了解析解,这在文献中是不可用的。数值结果突出了辐射声场的多谐性质,并提供了与表面动态变形相关的边界贡献分析。为了完整起见,还介绍了在多孔变形球形和翼状边界上的成功应用。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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